DE2136534C3 - Brennstoffblock fur Heißgas Hybrid Generatoren - Google Patents

Brennstoffblock fur Heißgas Hybrid Generatoren

Info

Publication number
DE2136534C3
DE2136534C3 DE2136534A DE2136534A DE2136534C3 DE 2136534 C3 DE2136534 C3 DE 2136534C3 DE 2136534 A DE2136534 A DE 2136534A DE 2136534 A DE2136534 A DE 2136534A DE 2136534 C3 DE2136534 C3 DE 2136534C3
Authority
DE
Germany
Prior art keywords
areas
block
fuel
partition
blocks
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
DE2136534A
Other languages
German (de)
English (en)
Other versions
DE2136534A1 (de
DE2136534B2 (de
Inventor
Claude Neauphle-Lechateau Verdier (Frankreich)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Office National dEtudes et de Recherches Aerospatiales ONERA
Ministere des Armees
Original Assignee
Office National dEtudes et de Recherches Aerospatiales ONERA
Ministere des Armees
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Office National dEtudes et de Recherches Aerospatiales ONERA, Ministere des Armees filed Critical Office National dEtudes et de Recherches Aerospatiales ONERA
Publication of DE2136534A1 publication Critical patent/DE2136534A1/de
Publication of DE2136534B2 publication Critical patent/DE2136534B2/de
Application granted granted Critical
Publication of DE2136534C3 publication Critical patent/DE2136534C3/de
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/12—Shape or structure of solid propellant charges made of two or more portions burning at different rates or having different characteristics
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/10—Shape or structure of solid propellant charges
    • F02K9/14—Shape or structure of solid propellant charges made from sheet-like materials, e.g. of carpet-roll type, of layered structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Solid Fuels And Fuel-Associated Substances (AREA)
  • Feeding And Controlling Fuel (AREA)
DE2136534A 1970-07-22 1971-07-21 Brennstoffblock fur Heißgas Hybrid Generatoren Expired DE2136534C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7027104A FR2096975B1 (enExample) 1970-07-22 1970-07-22

Publications (3)

Publication Number Publication Date
DE2136534A1 DE2136534A1 (de) 1972-02-03
DE2136534B2 DE2136534B2 (de) 1973-05-24
DE2136534C3 true DE2136534C3 (de) 1973-12-13

Family

ID=9059067

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2136534A Expired DE2136534C3 (de) 1970-07-22 1971-07-21 Brennstoffblock fur Heißgas Hybrid Generatoren

Country Status (4)

Country Link
US (1) US3779011A (enExample)
DE (1) DE2136534C3 (enExample)
FR (1) FR2096975B1 (enExample)
SE (1) SE365580B (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4643166A (en) * 1984-12-13 1987-02-17 The Garrett Corporation Steam engine reaction chamber, fuel composition therefore, and method of making and operating same
US4730601A (en) * 1984-12-13 1988-03-15 The Garrett Corporation Steam engine reaction chamber, fuel composition therefore, and method of making and operating same
US5101623A (en) * 1990-02-06 1992-04-07 Rockwell International Corporation Rocket motor containing improved oxidizer injector
CN101545416B (zh) * 2008-03-24 2010-12-15 沈阳理工大学 固体火箭发动机

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL261914A (enExample) * 1960-03-04
US3137126A (en) * 1961-01-11 1964-06-16 North American Aviation Inc Method and means for forming a gaseous passage
US3677010A (en) * 1964-03-11 1972-07-18 Us Army Rocket motor and method
US3267672A (en) * 1964-12-17 1966-08-23 James R Craig Gas generating device with initiator insulating means
FR1502732A (fr) * 1966-07-26 1967-11-24 Thomson Houston Comp Francaise Perfectionnements aux propulseurs spatiaux à poussée contrôlable
DE1571248B1 (de) * 1966-10-18 1970-06-04 Messerschmitt Boelkow Blohm Zweistufiges Verfahren zur Erzeugung von brennbaren,unter Druck stehenden Gasen fuer Triebwerke,insbesondere Raketen- und Staustrahltriebwerke
US3568448A (en) * 1969-04-01 1971-03-09 Thiokol Chemical Corp Ignition system for igniting a gas generator by the use of combustion gases from a solid propellant rocket motor having selective zoning capabilities

Also Published As

Publication number Publication date
US3779011A (en) 1973-12-18
FR2096975A1 (enExample) 1972-03-03
FR2096975B1 (enExample) 1974-05-03
DE2136534A1 (de) 1972-02-03
SE365580B (enExample) 1974-03-25
DE2136534B2 (de) 1973-05-24

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)
E77 Valid patent as to the heymanns-index 1977
8339 Ceased/non-payment of the annual fee